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Theoretical Study of the Low-Aspect-Ratio Wings in Uniform Shear Flow : The Case of the Free Stream Velocity Varying in the Spanwise Direction

机译：均匀剪切流动低纵横比翼的理论研究：枝条方向自由流速度变化的情况

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Kuninobu MORITA;
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年度 1969
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4. Flow Structures on a Low-Aspect-Ratio Wing Undergoing a Pitch-Ramp–Hold Manoeuvre in a Uniform Cross-Flow [C] . A. Agon, M. Giacobello, J. L. Palmer Australasian Fluid Mechanics Society;Australasian Fluid Mechanics Conference . 2014

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7. The Spanwise Non-Uniformity of Nominally Two-Dimensional Turbulent Boundary Layer : 2nd Report, Wall Shear Stress and Flow Field [O] . Yoshimasa FURUYA, Ikuo NAKAMURA, Hideo OSAKA, 1974

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Theoretical Study of the Low-Aspect-Ratio Wings in Uniform Shear Flow : The Case of the Free Stream Velocity Varying in the Spanwise Direction

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